| 发明名称 | Heat exchanger arrangement for turbine engine | ||
| 摘要 | A turbine engine cooling arrangement includes a core passage for receiving a core flow for combustion, a first airflow source including a first passage adjacent the core passage for conveying a first airflow, and a second airflow source including a second passage adjacent the first passage for conveying a second airflow. A heat exchanger is thermally connected with the first passage and the second passage for transferring heat between the first airflow and the second airflow. | ||
| 申请公布号 | US9212623(B2) | 申请公布日期 | 2015.12.15 |
| 申请号 | US200711964058 | 申请日期 | 2007.12.26 |
| 申请人 | United Technologies Corporation | 发明人 | Murphy Michael Joseph;Zamora Sean P. |
| 分类号 | F01D25/08;F02K1/46;F01D25/12;F01D25/14;F02K1/82;F04D29/58 | 主分类号 | F01D25/08 |
| 代理机构 | Carlson, Gaskey & Olds, P.C. | 代理人 | Carlson, Gaskey & Olds, P.C. |
| 主权项 | 1. A turbine engine cooling arrangement comprising: a core passage for receiving a core flow for combustion; a first airflow source including a first passage adjacent the core passage for conveying a first airflow; a second airflow source including a second passage adjacent the first passage for conveying a second airflow; and a heat exchanger that is thermally connected with the first passage and the second passage for transferring heat between the first airflow and the second airflow, wherein the entire first passage is located radially outwards of the core passage, and the entire second passage is located radially outwards of the first passage, relative to the core flow. | ||
| 地址 | Hartford CT US | ||